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Design of a 7kW power transfer solar array drive mechanismWith the availability of the Shuttle and the European launcher, Ariane, there will be a continuing trend towards large payload satellite missions requiring high-power, high-inertia, flexible solar arrays. The need arises for a solar array drive with a large power transfer capability which can rotate these solar arrays without disturbing the satellite body pointing. The modular design of such a Solar Array Drive Mechanism (SADM) which is capable of transferring 7kW of power or more is described. Total design flexibility has been achieved, enabling different spacecraft power requirements to be accommodated within the SADM design.
Document ID
19820015493
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sheppard, J. G.
(British Aerospace Dynamics Group Stevenage, United Kingdom)
Date Acquired
August 10, 2013
Publication Date
May 1, 1982
Publication Information
Publication: NASA. Kennedy Space Center The 16th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
82N23367
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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